High-Precision Control Strategy for Ultra-Low Speed and Variable Speed Motion of Satellite Platform Pointing Mechanisms

Satellite pointing mechanisms for earth observation require ultra-low speed scanning (approximately 70″/s) and precise variable-speed compensation. However, traditional Field-Oriented Control (FOC) suffers from significant velocity bias and instability under these conditions. To address these issues, this paper proposes a position-loop-based speed control scheme integrated with a variable structure control strategy. By substituting the speed command with a position loop, the proposed method effectively suppresses steady-state velocity bias, while the variable structure strategy mitigates fluctuations during variable-speed motion. Experimental results indicate that, compared to traditional FOC, the proposed method reduces velocity bias error by over 30% during uniform tracking and decreases the amplitude of velocity fluctuations by more than 40% in variable-speed scenarios. This strategy significantly enhances the control precision of satellite pointing mechanisms and improves on-orbit imaging compensation accuracy.

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Publication Details

Journal
Aerospace
Published
2026-01-25
DOI
https://doi.org/10.3390/aerospace13020118
Primary Topic
Inertial Sensor and Navigation
Type
article
Field-Weighted Citation Impact
0.00

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article

High-Precision Control Strategy for Ultra-Low Speed and Variable Speed Motion of Satellite Platform Pointing Mechanisms

Hui Li, Jianjun Jia, Xinyu Zhao, Yanfeng He et al.
Aerospace
Inertial Sensor and Navigation
article

High-Precision Control Strategy for Ultra-Low Speed and Variable Speed Motion of Satellite Platform Pointing Mechanisms

Hui Li, Jianjun Jia, Xinyu Zhao, Yanfeng He, Xindong Liang, C. M. Han, Xue Wang, Jiahao Cai, Zhenyu Fan, Jiayi Shen
article en

Abstract

Satellite pointing mechanisms for earth observation require ultra-low speed scanning (approximately 70″/s) and precise variable-speed compensation. However, traditional Field-Oriented Control (FOC) suffers from significant velocity bias and instability under these conditions. To address these issues, this paper proposes a position-loop-based speed control scheme integrated with a variable structure control strategy. By substituting the speed command with a position loop, the proposed method effectively suppresses steady-state velocity bias, while the variable structure strategy mitigates fluctuations during variable-speed motion. Experimental results indicate that, compared to traditional FOC, the proposed method reduces velocity bias error by over 30% during uniform tracking and decreases the amplitude of velocity fluctuations by more than 40% in variable-speed scenarios. This strategy significantly enhances the control precision of satellite pointing mechanisms and improves on-orbit imaging compensation accuracy.

AerospaceVol. 13(2)
Chinese Academy of Sciences (CN), Hefei Institutes of Physical Science (CN), Anhui Institute of Optics and Fine Mechanics (CN), Shanghai Institute of Technical Physics (CN), University of Chinese Academy of Sciences (CN)
Chinese Academy of Sciences, University of Chinese Academy of Sciences
Openalex Percentile: Top 80%
Inertial Sensor and Navigation
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